Common use of Climb Clause in Contracts

Climb. cruise and descent performance elements of the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in paragraph 7.3 below may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing. Cruise performance at 20,000 ft and above are based on a center of gravity position of 30% MAC.

Climb. cruise cruise, descent and descent holding performance elements of the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in paragraph 7.3 below may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing. Cruise performance at 20,000 ft and above are based on a center of gravity position of 30% * MAC.

Climb. cruise and descent performance elements of associated with the Guarantees will shall include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in paragraph 7.3 below Paragraph 8.3 may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will shall be bled from the engines for anti-icing. Cruise performance at 20,000 ft [DELETED]ft and above are is based on a center of gravity position of 30[DELETED] % MAC, unless otherwise stated.

Climb. cruise and descent performance elements of associated with the Guarantees will shall include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in paragraph 7.3 below Paragraph 10.3 may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will shall be bled from the engines for anti-icing. Cruise performance at 20,000 [DELETED] ft and above are is based on a center of gravity position of 30TBD % MAC, unless otherwise stated.

Climb. cruise and descent performance elements of the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in paragraph 7.3 6.3 below may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing. Cruise performance at 20,000 ft and above are based on a center of gravity position of 3034% MAC.

Climb. cruise and descent performance elements of associated with the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in paragraph 7.3 Subparagraph 8.3 below may be such as to optimize optimise the Aircraft performance while meeting the minimum normal air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing. Cruise performance at 20,000 ft and above are is based on a center centre of gravity position of 3034% MAC.

Climb. cruise and descent performance elements of the Guarantees will include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in paragraph 7.3 9.3 below may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will be bled from the engines for anti-icing. Cruise performance at 20,000 ft and above are based on a center of gravity position of 30% MAC.

Climb. cruise and descent performance elements of associated with the Guarantees will shall include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in paragraph 7.3 below Paragraph 9.3 may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will shall be bled from the engines for anti-icing. Cruise performance at 20,000 [DELETED] ft and above are is based on a center of gravity position of 30[DELETED] % MAC, unless otherwise stated.

Climb. cruise and descent performance elements of associated with the Guarantees will shall include allowances for normal electrical load and for normal engine air bleed and power extraction associated with maximum cabin differential pressure as defined in Section 21-30.31 of the Specification. Cabin air conditioning management during performance demonstration as described in paragraph 7.3 below Paragraph 8.3 may be such as to optimize the Aircraft performance while meeting the minimum air conditioning requirements defined above. Unless otherwise stated no air will shall be bled from the engines for anti-icing. Cruise performance at 20,000 [DELETED] ft and above are is based on a center of gravity position of 30[DELETED] % MAC, unless otherwise stated.